LEADER 01288nam2-2200373---450- 001 990003613910203316 005 20120120132048.0 010 $a978-3-406-62417-9 035 $a000361391 035 $aUSA01000361391 035 $a(ALEPH)000361391USA01 035 $a000361391 100 $a20120120d2011----km-y0itay50------ba 101 $ager 102 $aDE 105 $a||||||||001yy 200 1 $aAkteneinscicht und-auskünfte fur den Verlezten, Privatpersonem um sonstige Stellen §§ 406e und 475 StPO$fvon Carl Constantin Lauterwein 210 $aMünchen$cC.H. Beck$d2011 215 $aXXV, 288 p.$d24 cm 225 2 $aMünchener Universitätsschriften$v235 410 0$aMünchener Universitätsschriften$1001000334904$v, 235 454 1$12001 461 1$1001-------$12001 676 $a349.43 700 1$aLAUTERWEIN,$bCarl Constantin$0611379 801 0$aIT$bsalbc$gISBD 912 $a990003613910203316 951 $aXXX.A. Coll. 7/ 140$b71901 G.$cXXX.A. Coll. 7/$d00305531 959 $aBK 969 $aGIU 979 $aFIORELLA$b90$c20120120$lUSA01$h1318 979 $aFIORELLA$b90$c20120120$lUSA01$h1320 996 $aAkteneinscicht und-auskünfte fur den Verlezten, Privatpersonem um sonstige Stellen §§ 406e und 475 StPO$91137576 997 $aUNISA LEADER 01409nam 2200397Ia 450 001 9910700865303321 005 20110822150811.0 035 $a(CKB)5470000002412363 035 $a(OCoLC)747503958 035 $a(EXLCZ)995470000002412363 100 $a20110822d2011 ua 0 101 0 $aeng 135 $aurbn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aNumerical prediction of supersonic shock-boundary layer interaction$b[electronic resource] /$fVishal A. Bhagwandin and James DeSpirito 210 1$aAberdeen Proving Ground, MD :$cArmy Research Laboratory,$d[2011] 215 $a1 online resource (viii, 36 pages) $ccolor illustrations 225 1 $aARL-TR ;$v5602 300 $aTitle from title screen (viewed on Aug. 19, 2011). 300 $a"July 2011." 320 $aIncludes bibliographical references (pages 32-33). 606 $aShock waves$xResearch 606 $aAerospace engineering$xResearch 615 0$aShock waves$xResearch. 615 0$aAerospace engineering$xResearch. 700 $aBhagwandin$b Vishal A$01420296 701 $aDeSpirito$b James$01400611 712 02$aU.S. Army Research Laboratory. 801 0$bGPO 801 1$bGPO 906 $aBOOK 912 $a9910700865303321 996 $aNumerical prediction of supersonic shock-boundary layer interaction$93537693 997 $aUNINA